Publication Type Journal Article
Title On the Global and Localised Corrosion Behaviour of the AA2524-T3 Aluminium Alloy Used as Aircraft Fuselage Skin
Authors Jeferson Aparecido Moreto Luciana Sgarbi Rossino Waldek Wladimir Bose Filho Claudia Eliana Bruno Marino Miguel da Conceicao Ferreira Maryna Taryba JCS Fernandes
Groups CSSE
Journal MATERIALS RESEARCH-IBERO-AMERICAN JOURNAL OF MATERIALS
Year 2019
Month
Notice: Undefined index: in /afs/ist.utl.pt/groups/cqe/web/tmp/templates_c/77f86a5f762542dadf50c7f7fefa96acd45c2726_0.file.paper.tpl.html.php on line 163
Volume 22
Number 2
Pages
Abstract The aim of this work was to study the corrosion process of new aluminium alloy AA2524-T3 (Solution Heat Treated and Cold Worked), which is a promising substitute of the base line AA2024-T3 for aircrafts fabrication, by global and localised techniques in sodium chloride medium (0.05 mol L-1 NaCl). The open circuit potential results revealed a stochastic evolution of pitting events and to the resulting variations in the ratio of passive/active areas and/or cathode/anode, which may be related to the presence of different types of intermetallics. The cyclicvoltammetry showed that the corrosion potential (E-corr) and the pit nucleation potential (E-pit) values are quite similar (approximately -0.525 V). The results of EIS show that the corrosion rate is quite stable, with no tendency to increase or decrease for longer immersion periods. The results of SVET were in agreement with the results obtained by EIS technique, showing strong anodic activity on the surface with no repassivation along the whole immersion time. Besides, corrosion process led to significant surface degradation after 24h.
DOI http://dx.doi.org/10.1590/1980-5373-MR-2018-0280
ISBN
Publisher
Book Title
ISSN 1516-1439
EISSN 1980-5373
Conference Name
Bibtex ID ISI:000456946100001
Observations
Back to Publications List